Vibration Control of an Engine Mount for UAV Activated by Piezostack Actuator

被引：0

作者：

Oh, Jong-Seok ^{[1
]}

Choi, Seung-Bok ^{[1
]}

机构：

[1] Inha Univ, Dept Mech Engn, Inchon 402751, South Korea

来源：

ADVANCES IN MECHANICAL ENGINEERING, PTS 1-3 | 2011年 / 52-54卷

关键词：

Unmanned Aerial Vehicle (UAV); Engine Mount; Piezostack Actuator; Active Vibration Control; Sliding Mode Controller;

D O I：

10.4028/www.scientific.net/AMM.52-54.358

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

In this paper, vibration control performance of piezostack active engine mount system for unmanned aero vehicle (UAV) is evaluated via computer simulation. As a first step, the dynamic model of engine mount system which is supported at three points is derived. In the configuration of engine mount system, the inertia type of piezostack based active mount is installed for active vibration control. Then, the vibration level of UAV engine is measured. To attenuate the vibration which is transmitted from engine, a sliding mode controller which is robust to uncertain parameters is designed. Vibration control performances of active engine mount system are evaluated at each mount and center of gravity. Effective Control results are presented in both time and frequency domains.

引用

页码：358 / 364

页数：7

共 50 条

[21] ACTIVE VIBRATION CONTROL OF A STIFFENED PLATE WITH A PIEZOELECTRIC ACTUATOR [J].

Zhang, Ya-hong ;

Zhang, Xi-nong .

2011 SYMPOSIUM ON PIEZOELECTRICITY, ACOUSTIC WAVES AND DEVICE APPLICATIONS (SPAWDA), 2011, :264-268

[22] Vibration transmission control of vibration source in a cylindrical shell based on piezoelectric actuator [J].

He P. ;

Wang S. ;

Geng X. ;

Xie X. ;

Zhang Z. .

Zhendong yu Chongji/Journal of Vibration and Shock, 2024, 43 (01) :246-251

[23] Summarisation, Simulation and Comparison of Nine Control Algorithms for an Active Control Mount with an Oscillating Coil Actuator [J].

Fan, Rang-Lin ;

Wang, Pu ;

Han, Chen ;

Wei, Li-Jun ;

Liu, Zi-Jian ;

Yuan, Pei-Ju .

ALGORITHMS, 2021, 14 (09)

[24] Cascaded Trajectory Tracking Control for A Quadcopter UAV with Consideration of Actuator Dynamics [J].

Huang, Wenbin ;

Huang, Jing ;

Wang, Ban ;

Zhang, Yulong ;

Zhang, Youmin .

2022 41ST CHINESE CONTROL CONFERENCE (CCC), 2022, :2848-2853

[25] Dynamic Performance and Optimal Control Method Study on MRF Engine Mount [J].

Hou, Suojun ;

Shi, Wenku ;

Mao, Yang ;

Li, Haisheng .

2012 2ND INTERNATIONAL CONFERENCE ON APPLIED ROBOTICS FOR THE POWER INDUSTRY (CARPI), 2012, :283-287

[26] Control Strategy for Starter Generator in UAV with Micro Jet Engine [J].

Itoh, Jun-ichi ;

Kawamura, Kazuki ;

Koshikizawa, Hiroyuki ;

Abe, Kazuyuki .

2018 INTERNATIONAL POWER ELECTRONICS CONFERENCE (IPEC-NIIGATA 2018 -ECCE ASIA), 2018, :1567-1574

[27] Application of LIPCA as actuator for active vibration control of dynamic structures [J].

Suhariyono, A ;

Goo, NS ;

Park, HC ;

Yoon, KJ .

SMART STRUCTURES AND MATERIALS 2005: DAMPING AND ISOLATION, 2005, 5760 :510-517

[28] Development and experimental consideration of SMA/CFRP actuator for vibration control [J].

Yuse, K ;

Kikushima, Y .

SENSORS AND ACTUATORS A-PHYSICAL, 2005, 122 (01) :99-107

[29] Giant magnetostrictive actuator and its application in active vibration control [J].

Xu, HB ;

Zhang, TL ;

Jiang, CB ;

Zhang, H .

PRICM 5: THE FIFTH PACIFIC RIM INTERNATIONAL CONFERENCE ON ADVANCED MATERIALS AND PROCESSING, PTS 1-5, 2005, 475-479 :2089-2094

[30] Vibration control of a cantilever beam using distributed PVDF actuator [J].

Pereira, D ;

Shankar, VN ;

Sathiyanaarayan, S ;

Rao, CL ;

Sivakumar, SM .

SMART MATERIALS, STRUCTURES, AND SYSTEM, PTS 1 AND 2, 2003, 5062 :598-604

← 1 2 3 4 5 →